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S66286 Stainless Steel vs. 7076 Aluminum

S66286 stainless steel belongs to the iron alloys classification, while 7076 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is S66286 stainless steel and the bottom bar is 7076 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 17 to 40
6.2
Fatigue Strength, MPa 240 to 410
170
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 75
27
Shear Strength, MPa 420 to 630
310
Tensile Strength: Ultimate (UTS), MPa 620 to 1020
530
Tensile Strength: Yield (Proof), MPa 280 to 670
460

Thermal Properties

Latent Heat of Fusion, J/g 300
380
Maximum Temperature: Mechanical, °C 920
170
Melting Completion (Liquidus), °C 1430
630
Melting Onset (Solidus), °C 1370
460
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 15
140
Thermal Expansion, µm/m-K 17
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.9
35
Electrical Conductivity: Equal Weight (Specific), % IACS 2.2
100

Otherwise Unclassified Properties

Base Metal Price, % relative 26
9.5
Density, g/cm3 7.9
3.0
Embodied Carbon, kg CO2/kg material 6.0
8.0
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 170
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 150 to 200
31
Resilience: Unit (Modulus of Resilience), kJ/m3 190 to 1150
1510
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 22 to 36
49
Strength to Weight: Bending, points 20 to 28
48
Thermal Diffusivity, mm2/s 4.0
54
Thermal Shock Resistance, points 13 to 22
23

Alloy Composition

Aluminum (Al), % 0 to 0.35
86.9 to 91.2
Boron (B), % 0.0010 to 0.010
0
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 13.5 to 16
0
Copper (Cu), % 0
0.3 to 1.0
Iron (Fe), % 49.1 to 59.5
0 to 0.6
Magnesium (Mg), % 0
1.2 to 2.0
Manganese (Mn), % 0 to 2.0
0.3 to 0.8
Molybdenum (Mo), % 1.0 to 1.5
0
Nickel (Ni), % 24 to 27
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
0 to 0.4
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 1.9 to 2.4
0 to 0.2
Vanadium (V), % 0.1 to 0.5
0
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.15